Robust Velocity and Height Control for Uncertain Hypersonic Vehicles

被引:0
|
作者
Yu Lingyi [1 ]
Li Zhaoying [1 ]
Liu Hao [1 ]
Yu Yao [2 ]
机构
[1] Beihang Univ, Sch Astronaut, Beijing 100191, Peoples R China
[2] Univ Sci & Technol Beijing, Sch Automat & Elect Engn, Beijing 100083, Peoples R China
关键词
Hypersonic vehicle; nonlinear system; robust control; H-infinity control; TRACKING-CONTROL; NONLINEAR CONTROL; DESIGN; HELICOPTER; AIRCRAFT;
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper presents a robust controller design approach for the longitudinal dynamics of hypersonic vehicles. The proposed linear and time-invariant controller includes a state feedback H-infinity controller and a robust compensator. The robust compensator is introduced to restrain the effects of nonlinear dynamics and unstructured uncertainties in the whole frequency range. It is proven that the velocity and height tracking errors can be guaranteed to converge to the neighborhood of the origin in a finite time. Simulation results are given to show the advantages of the proposed control method.
引用
收藏
页码:2297 / 2302
页数:6
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